Model: 68A116109-2035

Aircraft Spar

Special Features:

Opposite -2036; replaces -2029; nha 68a116119

Properties:

Overall Length
83.000 inches
Overall Width
4.000 inches
Material Thickness
3.750 inches
Aircraft Location
Outbd trailing edge closure spar
Aircraft Mission Design Series
F-15
Material
Aluminum alloy 7175
Material Specification
Mms1304 federal specification single material response
NSN
1560-01-260-1081
Part Number
68A116109-2035
Description
Spar,aircraft
CAGE
76301

A principal spanwise member of the structural framework of a wing, stabilizer, other airfoil, and the like. It is designed to absorb bending loads applied to the airfoil.

Part 68A116109-2035 NSN 1560-01-260-1081

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
41028
FIIG:
A11400
Concept No.:
App. Key:
A
Cond. Code:
1
Status:
A

Material Classification

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
P
PMIC:
A
ESD:
ESD:
MMAC:
FX
CRITL:
X

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
19.0000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
E
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
011790
UFC:
04720
LTL:
RATING VARIABLE
LCL:
--
WCC:
671
TCC:
Z
SHC:
9
ACC:
Equipment for Aircraft

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Schedule B and Export
  • Schedule B: 8803909060
  • SITC: 79297
  • End Use: Parts for military-type goods
  • NAICS: 336419
  • USDA: 1

Freight Class: Other parts, nesoi, for use in other military aircraft, spacecraft and spacecraft launch vehicles (excluding parts of communication satellites)

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